- do a check of the wiring of the RUD TR RES NO MON discrete (from the FAC 1 (1CC1) to the RUD TRIM/RESET pushbutton switch (8CC)) (Ref. ASM 22-68/03).
(a) If there is no continuity:
- repair the above wiring.
(b) If there is continuity:
- do a check and repair the wiring of the ground signal at RUD TRIM/RESET pushbutton switch (8CC) (from pin 8 to the first terminal block) (Ref. ASM 22-68/03).
B. If only the second test gives the maintenance message AFS : FAC1/RT RESET SW 8CC:
- replace the FAC 1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(1) If the fault continues:
- replace the P/BSW-RUD TRIM/RESET (8CC).
(2) If the fault continues:
- do a check of the wiring of the RUD TR RES NC COM discrete (from the FAC 1 (1CC1) to the RUD TRIM/RESET pushbutton switch (8CC)) (Ref. ASM 22-68/03).
(a) If there is no continuity:
- repair the above wiring.
(b) If there is continuity:
- do a check and repair the wiring of the ground signal at RUD TRIM/RESET pushbutton switch (8CC) (from pin 2 to the first terminal block) (Ref. ASM 22-68/03).
C. If the two tests give the maintenance message AFS : FAC1/RT RESET SW 8CC:
- do a check and repair the wiring of the ground signal from the ground point to the first terminal block (Ref. ASM 22-68/03).
D. Do the tests given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞22-62-00∞∞∞∞∞∞∞∞∞∞Page 226
May 01/98R
CES Failure of the Rudder Trim/Reset Circuit of the FAC 2
1. Possible Causes
_______________
- FAC-2 (1CC2)
- P/BSW-RUD TRIM/RESET (8CC)
- wiring of the RUD TR RES NO MON discrete (from the FAC 2 (1CC2) to the RUD TRIM/RESET pushbutton switch (8CC))
- wiring of the ground signal at RUD TRIM/RESET pushbutton switch (8CC)
- wiring of the RUD TR RES NC COM discrete (from the FAC 2 (1CC2) to the RUD TRIM/RESET pushbutton switch (8CC))
- wiring of the ground signal
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 22-66-34-000-002 Removal of the FAC (1CC1,1CC2)
AMM 22-66-34-400-002 Installation of the FAC (1CC1,1CC2)
AMM 22-96-00-710-001 Operational Test of the AFS
ASM 22-68/03
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) and read the result for the FAC2:
(a) With the RUD TRIM/RESET pushbutton switch (8CC) pushed.
(b) With the RUD TRIM/RESET pushbutton switch (8CC) released.
4. Fault Isolation
_______________
A. If only the first test gives the maintenance message AFS : FAC2/RT RESET SW 8CC:
- replace the FAC-2 (1CC2), (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(1) If the fault continues:
- replace the P/BSW-RUD TRIM/RESET (8CC).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞22-62-00∞∞∞∞∞∞∞∞∞∞Page 227
May 01/98R
CES (2) If the fault continues:
- do a check of the wiring of the RUD TR RES NO MON discrete (from the FAC 2 (1CC2) to the RUD TRIM/RESET pushbutton switch (8CC)) (Ref. ASM 22-68/03).
(a) If there is no continuity:
- repair the above wiring.
(b) If there is continuity:
- do a check and repair the wiring of the ground signal at RUD TRIM/RESET pushbutton switch (8CC) (from pin 4 to the first terminal block) (Ref. ASM 22-68/03).
B. If only the second test gives the maintenance message AFS : FAC2/RT RESET SW 8CC:
- replace the FAC 2 (1CC2) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(1) If the fault continues:
- replace the P/BSW-RUD TRIM/RESET (8CC).
(2) If the fault continues:
- do a check of the wiring of the RUD TR RES NC COM discrete (from the FAC 2 (1CC2) to the RUD TRIM/RESET pushbutton switch (8CC)) (Ref. ASM 22-68/03).
(a) If there is no continuity:
- repair the above wiring.
(b) If there is continuity: 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AUTO FLIGHT 自動飛行1(101)
